Department of Transportation 2012 – Federal Register Recent Federal Regulation Documents

We propose to supersede an existing airworthiness directive (AD) that applies to certain The Boeing Company Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, 747SR, and 747SP series airplanes; and certain Model 757-200, -200PF, and -300 series airplanes. The existing AD currently requires replacing the control switches of the forward, aft, and nose cargo doors for certain airplanes, and replacing the control switches of cargo doors 1 and 2 for certain airplanes. Since we issued that AD, we have determined that additional airplanes are affected by the identified unsafe condition. This proposed AD would continue to require replacing the control switches of the forward, aft, and nose cargo doors of Model 747 airplanes; and the control switches of cargo doors 1 and 2 of Model 757 airplanes; this proposed AD also adds airplanes to the applicability and revises the initial compliance times. We are proposing this AD to prevent injuries to persons and damage to the airplane and equipment.

This action amends Class E airspace at Sweetwater, TX. Additional controlled airspace is necessary to accommodate new Area Navigation (RNAV) Standard Instrument Approach Procedures at Avenger Field Airport. The airport's geographic coordinates are adjusted and the airport name changed. The FAA is taking this action to enhance the safety and management of Instrument Flight Rule (IFR) operations at the airport.

FMCSA announces that MCSAC will hold a meeting on Monday- Wednesday, August 27-29, 2012. On Monday, August 27, 2012, MCSAC will be provided with briefings on the major motor carrier safety provisions of the recently enacted Moving Ahead for Progress in the 21st Century (MAP-21) [Pub. L. 112-140] surface transportation act and the Agency's Compliance, Safety, and Accountability (CSA) program and assigned a new task concerning CSA. Additionally, the MCSAC will establish a subcommittee on CSA to provide concepts, ideas, and recommendations on the program. On Monday afternoon, the Cross-Border Trucking Pilot Subcommittee will convene for a status update from the Agency. On Tuesday, August 28, 2012, MCSAC will be given a new task to provide ideas and concepts concerning the Regulatory Flexibility Act Section 610 review process and will hear presentations on that topic. Wednesday morning, August 29, 2012, will be reserved for MCSAC's Motorcoach Hours-of-Service (HOS) subcommittee. All three days of the meeting will be open to the public.

This notice announces the Twentieth Public Meeting of members of the Crash Injury Research and Engineering Network. CIREN is a collaborative effort to conduct research on crashes and injuries at six Level I Trauma Centers across the United States linked by a computer network. The current CIREN model utilizes two types of centers, medical and engineering. Medical centers are based at Level I Trauma Centers that admit large numbers of people injured in motor vehicle crashes. These teams are led by trauma surgeons and emergency physicians and also include a crash investigator and project coordinator. Engineering centers are based at academic engineering laboratories that have experience in motor vehicle crash and human injury research. Engineering teams partner with trauma centers to enroll crash victims into the CIREN program. Engineering teams are led by mechanical engineers, typically trained in the area of impact biomechanics. Engineering teams also include trauma/emergency physicians, a crash investigator, and a project coordinator. Either type of team typically includes additional physicians and/or engineers, epidemiologists, nurses, and other researchers. The CIREN process combines prospective data collection with professional multidisciplinary analysis of medical and engineering evidence to determine injury causation in every crash investigation conducted. Researchers can review data and share expertise, which may lead to a better understanding of crash injury mechanisms and the design of safer vehicles. The six centers will give presentations on current research based on CIREN data. Topics include thoraco-lumbar fractures in frontal crashes, risk of pelvic fractures in motor vehicle collisions, trauma system adoption of Advanced Automatic Collision Notification (AACN) Systems, lower extremity injury patterns sustained in frontal crashes, evaluation of brain lesion location sustained in motor vehicle crashes, and major vascular injuries. The final agenda will be posted to the CIREN Web site that can be accessed by going to the NHTSA homepage https://www.nhtsa.dot.gov/, click on Vehicle Safety Research on the right side of the top toolbar, and then click on Crash Injury Research and Engineering Network (CIREN) in the box on the left. The agenda will be posted one week prior to the meeting.

FMCSA provides notice of the Agency's policy concerning review of applications for operating authority registration, and suspension, amendment or revocation of existing operating authority registration. Motor carriers, brokers and freight forwarders must demonstrate a willingness and ability to comply with applicable statutes and regulations in order to obtain and maintain operating authority registration. This notice outlines FMCSA's policy for evaluating motor carriers', brokers' and freight forwarders' willingness and ability to comply with these requirements.

This action proposes to amend Class E airspace at Ontonagon, MI. Additional controlled airspace is necessary to accommodate new Standard Instrument Approach Procedures (SIAP) at Ontonagon County- Schuster Field Airport. Also, this action would rename the airport. The FAA is taking this action to enhance the safety and management of Instrument Flight Rules (IFR) operations for SIAPs at the airport.

This action proposes to amend Class E airspace at Guthrie, IA. Decommissioning of the Guthrie Center non-directional radio beacon (NDB) at Guthrie County Regional Airport, Guthrie, IA, has made this action necessary for the safety and management of Instrument Flight Rules (IFR) operations at the airport. Geographic coordinates of the airport would also be adjusted.

FMCSA announces its decision to renew the exemptions from the vision requirement in the Federal Motor Carrier Safety Regulations for 48 individuals. FMCSA has statutory authority to exempt individuals from the vision requirement if the exemptions granted will not compromise safety. The Agency has concluded that granting these exemption renewals will provide a level of safety that is equivalent to or greater than the level of safety maintained without the exemptions for these commercial motor vehicle (CMV) drivers.

In accordance with the Paperwork Reduction Act of 1995, PHMSA invites comments on two information collections that we will be submitting to the Office of Management and Budget (OMB) for renewal. The information collections relate to the pipeline integrity management requirements for gas transmission pipeline operators and the response plan requirements for operators of onshore oil pipelines. A Federal Register Notice with a 60-day comment period soliciting comments on the following information collection was published in the Federal Register on May 9, 2012, (77 FR 27279) under Docket No. PHMSA-2012-0094. No comments were received. The purpose of this notice is to allow the public an additional 30 days to submit comments to OMB on the information collection described below.

We propose to adopt a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This proposed AD was prompted by cases of on-ground failure of the screw cap or end cap of hydraulic accumulators on other airplane models, resulting in high-energy impact damage to adjacent systems and structure. This proposed AD would require inspecting for a part number and replacing the affected parking brake hydraulic accumulator, and relocating the parking brake accumulator, on the subject airplanes. We are proposing this AD to prevent failure of the screw caps and/or end caps of the parking brake hydraulic accumulator, which could result in damage to the airplane's primary structures, with potential adverse effect on the airplane's controllability.

This rule establishes, amends, suspends, or revokes Standard Instrument Approach Procedures (SIAPs) and associated Takeoff Minimums and Obstacle Departure Procedures for operations at certain airports. These regulatory actions are needed because of the adoption of new or revised criteria, or because of changes occurring in the National Airspace System, such as the commissioning of new navigational facilities, adding new obstacles, or changing air traffic requirements. These changes are designed to provide safe and efficient use of the navigable airspace and to promote safe flight operations under instrument flight rules at the affected airports.

The Department of Transportation is directing all interested persons to show cause why it should not issue an order finding Key Lime Air Corporation fit, willing, and able, and awarding it a Commuter Air Carrier Authorization.

We propose to adopt a new airworthiness directive (AD) for certain The Boeing Company Model MD-90-30 airplanes. This proposed AD was prompted by reports of fatigue cracks found in Stringer 11 at the outboard flap, inboard drive hinge at Station Xrs=164.000. This proposed AD would require repetitive inspections for cracks in Stringer 11, and a splice repair if necessary; and repetitive post-repair inspections, and repair if necessary. We are proposing this AD to detect and correct such cracking, which could result in the wing structure not supporting the limit load condition, which could lead to loss of the structural integrity of the wing.

Pursuant to the recently enacted Moving Ahead for Progress in the 21st Century Act (MAP-21), DOT announces the availability of funding authorized in the amount of $1.75 billion ($750 million in Federal Fiscal Year (FY) 2013 funds and $1 billion in FY 2014 funds (and any funds that may be available from prior fiscal years)) to provide TIFIA credit assistance for eligible projects. The FY 2013 and FY 2014 funds are subject to an annual obligation limitation that may be established in appropriations law. The amount of TIFIA budget authority available in a given year may be less than the amount authorized for that fiscal year. Under TIFIA, DOT provides secured (direct) loans, lines of credit, and loan guarantees to public and private applicants for eligible surface transportation projects. Projects must meet statutorily specified eligibility criteria to receive credit assistance. This notice outlines the process that project sponsors must follow in seeking TIFIA credit assistance. DOT is publishing this notice to give project sponsors an opportunity to submit Letters of Interest for the newly authorized funding as soon as possible. However, in addition to authorizing more funding for TIFIA credit assistance, MAP-21 made some significant changes to the TIFIA program's structure, including the terms and conditions pursuant to which DOT can provide TIFIA credit assistance. While this notice provides guidance about how DOT will implement some of the changes made by MAP-21, it does not provide guidance about how DOT will implement all of these changes. Further information about the changes made by MAP-21 and additional DOT guidance for implementation of these provisions is provided in Part VII below. Also, Part VII invites interested parties to submit comments about DOT's implementation of MAP-21 and DOT's guidance for awarding TIFIA credit assistance. Unless otherwise noted, statutory section references in this notice are to sections of title 23 of the U.S. Code, as amended by MAP-21, which takes effect on October 1, 2012. Letter of Interest Submission: All project sponsors wishing to apply for TIFIA credit assistance must first submit a Letter of Interest, as more fully described in this notice of funding availability. Letters of Interest will be received on a rolling basis commencing on the date hereof, using the form on the TIFIA Web site: https://www.fhwa.dot.gov/ipd/tifia/guidance_applications/index .htm. Project sponsors that have previously submitted Letters of Interest for a prior fiscal year's funding, but have not been asked by DOT to submit an application as of the date of this notice, must submit a new Letter of Interest to be considered for the funding described in this notice of funding availability. Addresses for Letters of Interest: Submit all Letters of Interest to the attention of Mr. Duane Callender via email at: TIFIACredit@dot.gov. Submitters should receive a confirmation email, but are advised to request a return receipt to confirm transmission. Only Letters of Interest received via email, as provided above, shall be deemed properly filed. Addresses for Comments: You must include the agency name (Office of the Secretary of Transportation) and the docket number DOT-OST-2012- 0130 with your comments. To ensure your comments are not entered into the docket more than once, please submit comments, identified by the docket number DOT-OST-2012-0130, by only one of the following methods: Web site: The U.S. Government electronic docket site is www.regulations.gov. Go to this Web site and follow the instructions for submitting comments into docket number DOT-OST-2012-0130; Fax: Telefax comments to: 202-366-2908. Mail: Mail your comments to U.S. Department of Transportation, 1200 New Jersey Avenue SE., Docket Operations, M-30, Room W12-140, Washington, DC 20590; or Hand Delivery: Bring your comments to the U.S. Department of Transportation, 1200 New Jersey Avenue SE., Docket Operations, M-30, West Building Ground Floor, Room W12-140, Washington, DC 20590, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. Instructions for Submitting Comments: You must include the agency name (Office of the Secretary of Transportation) and Docket number DOT- OST-2012-0130 for this notice at the beginning of your comments. You should submit two copies of your comments if you submit them by mail or courier. For confirmation that the Office of the Secretary of Transportation has received your comments you must include a self- addressed stamped postcard. Note that all comments received will be posted without change to www.regulations.gov, including any personal information provided, and will be available to Internet users. You may review the Department's complete Privacy Act Statement in the Federal Register published April 11, 2000 (65 FR 19477), or you may visit www.regulations.gov.

This action proposes to modify the Philadelphia, PA, Class B airspace area to ensure the containment of large turbine-powered aircraft within Class B airspace, reduce controller workload, and reduce the potential for midair collision in the Philadelphia terminal area.

We propose to adopt a new airworthiness directive (AD) for certain Bombardier, Inc. Model CL-600-1A11 (CL-600), CL-600-2A12 (CL- 601), CL-600-2B16 (CL-601-3A, CL-601-3R, & CL-604 Variants) airplanes. This proposed AD was prompted by reports of cracking found on the upper and lower web of the engine support beam. This proposed AD would require revising the maintenance program. We are proposing this AD to detect and correct fatigue cracking of the engine support beam, which could result in failure of the engine support beam and affect the structural integrity of the airplane.

This action establishes Class E Airspace at Quakertown, PA, to accommodate the new Area Navigation (RNAV) Global Positioning System (GPS) Standard Instrument Approach Procedures at Quakertown Airport. This action enhances the safety and airspace management of Instrument Flight Rules (IFR) operations within the National Airspace System.

This action amends the Class E airspace area at Bar Harbor, ME, as the Surry Non-Directional Radio Beacon (NDB) has been decommissioned and new Standard Instrument Approach Procedures have been developed at Hancock County-Bar Harbor Airport. This action enhances the safety and airspace management of Instrument Flight Rules (IFR) operations within the National Airspace System. This action also makes a minor adjustment to the geographic coordinates of the airport.

In accordance with the National Environmental Policy Act (NEPA), 42 U.S.C. 4321-4347, and the Council on Environmental Quality NEPA implementing regulations, 40 CFR Parts 1500-1508, the Pipeline and Hazardous Materials Safety Administration (PHMSA) is announcing the availability of and requesting comments on the Draft Environmental Assessment (Draft EA) for the Longhorn Pipeline Reversal Project (Proposed Project).

This action amends Class D and E Airspace at Fort Rucker, AL, by updating the geographic coordinates of Cairns Army Air Field to aid in the navigation of our National Airspace System. This action is necessary for the continued safety and management of instrument flight rules (IFR) operations within the Fort Rucker, AL airspace area.

Pursuant to Section 10(a)(2) of the Federal Advisory Committee Act (Pub. L. 92-463, 5 U.S.C. App. 2), notice is hereby given of three teleconferences of the Systems Working Group of the Commercial Space Transportation Advisory Committee (COMSTAC). The teleconferences will take place on: Tuesday August 14, 2012, Tuesday September 18, 2012, and Tuesday October 23, 2012. All teleconferences will begin at 1:00 p.m. Eastern Daylight Time and will last approximately one hour. Individuals who plan to participate should contact Susan Lender, Designated Federal Officer (DFO), (the Contact Person listed below) by phone or email for the teleconference call in number. The purpose of these three teleconferences is to assist the FAA early in its development of regulations to protect occupants of commercial suborbital and orbital spacecraft. Although the FAA has not yet targeted a date for proposing regulations to protect the health and safety of crew and space flight participants, the FAA believes that the development of sound and appropriate regulations for human space flight can only be achieved with a deliberate, multi-year effort. Moreover, the FAA believes that early industry input into this regulatory effort before any formal proposal by the FAA is critical. Thus, the FAA would like to engage with COMSTAC on a periodic basis, approximately once per month, on specific topics. The topics for the first three teleconferences are as follows: (1) What Level of Safety Should FAA Target? We will discuss whether the FAA should regulate to one or multiple levels of space flight safety, what level or levels of safety the FAA should attempt to achieve, and whether the level or levels of safety should be quantified. We will also discuss what level of care, short of a fatality, the FAA should be concerned with. (2) What Should FAA Oversight Look Like? Aircraft-like certification is not feasible at this time, due to current technology and the FAA's statutory mandate only to pursue minimal regulations that take into consideration the evolving standards of safety in the commercial space flight industry. 51 U.S.C. 50905(c)(3). We will discuss what a licensing process should look like in terms of FAA oversight, whether such oversight could or should be called a ``certification,'' and for how long informed consent should remain in effect. (3) What Types of Requirements and Associated Guidance Material Should FAA Develop? In general, the FAA favors space transportation regulations that are performance or process based. We will discuss the level of empirical or analytical data necessary to justify any performance-based human space flight regulation, the possible use of Advisory Circulars to add clarity to regulations, and what place government and industry standards should have in FAA licensing. Interested members of the public may submit relevant written statements for the COMSTAC working group members to consider under the advisory process. Statements may concern the issues and agenda items mentioned above or additional issues that may be relevant for the U.S. commercial space transportation industry. Interested parties wishing to submit written statements should contact Susan Lender, DFO, (the Contact Person listed below) in writing (mail or email) by August 7, 2012, for the August 14 teleconference, September 11, 2012, for the September 18 teleconference, and October 16, 2012, for the October 23 teleconference. This way the information can be made available to COMSTAC members for their review and consideration before each teleconference. Written statements should be supplied in the following formats: one hard copy with original signature or one electronic copy via email. The FAA may schedule up to 10 more teleconferences in the coming months to allow the U.S. commercial space transportation industry to share views with the FAA on a number of specific topics related to commercial human space flight safety. An agenda will be posted on the FAA Web site at https://www.faa.gov/ go/ast. Individuals who plan to participate and need special assistance should inform the Contact Person listed below in advance of the meeting.

We propose to adopt a new airworthiness directive (AD) for Eurocopter France (Eurocopter) Model AS350B3 and EC130B4 helicopters. This proposed AD would require revising the Limitations section of the Rotorcraft flight Manual (RFM) to reduce the starter generator operating current to 180 amperes (amps) and installing a placard in the instrument panel indicating the revised limitation. This proposed AD is prompted by the determination that the manufacturer-installed Aircraft Parts Corporation (APC) starter generator has exceeded the shaft horse power extractions allowed for Turbomeca engines. The proposed actions are intended to prevent the engine surge margin being reduced, which can result in engine failure.

We propose to adopt a new airworthiness directive (AD) for Eurocopter France (Eurocopter) Model AS332C, L, and L1 helicopters to require a one-time inspection of the main rotor head (MRH) swash-plate upper bearing (bearing) for a non-smooth point (friction point). This proposed AD is prompted by a report of the premature deterioration of the MRH bearing of the rotating star installed on a Model AS332L1 helicopter. The proposed actions are intended to detect deterioration of the MRH bearing and to prevent overloading the scissor links which drive the main rotor system, failure of the scissors links, and subsequent loss of control of the helicopter.